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Jia Wang Yu

from Baldwin Park, CA
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Related to:
Chao Y Wang-Klein, 66Changjin J WangChristopher York Yang, 52Thalinee Wang, 48Yu Lian YuGeay F WangMark X Wang, 57
Connected to:
Abigail M Yu, 43Adeline Y Yu, 40Ai Yu, 64Aimy Yu, 30Aiping A Yu, 71Alisa Yu, 34Allen Yu, 30Angelia W Yu, 74Angelita T Yu, 68Anna Yu, 56

Jia Yu Phones & Addresses

  • Baldwin Park, CA
  • Baldwin Park, CA
  • 3422 Stichman Ave, Baldwin Park, CA 91706

Professional Records

Lawyers & Attorneys

Jia Yu Photo 1

Jia Yu - Lawyer

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Specialties:
Litigation
Corporate & Incorporation
ISLN:
1000639170
Admitted:
2009

Business Records

Name / Title
Company / Classification
Phones & Addresses
Jia Rui Yu
Director
Yu's Chopstix Inc
Jia Yu
Principal
Legend Solutions
Business Services
3422 Stichman Ave, Duarte, CA 91706
Jia Lu Yu
YOGURT CITY BRUNSWICK INC
Jia Lu Yu
CHINA HOUSE (USA) INC
Jia Lu Yu
CHINA HOUSE, INC
Jia Yu
President
YING LI INTERNATIONAL
Nonclassifiable Establishments
500 Cameron Crst Dr, Diamond Bar, CA 91765

Publications

Wikipedia

Jia Yu Channel

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Jia Yu Channel (Chinese: , pinyin: jiy pndo) is a 24-hour Mandarin and Cantonese subscription channel in Malaysia, broadcasting under the ...

Us Patents

Acoustic Barrel For Aircraft Engine Nacelle Including Crack And Delamination Stoppers

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US Patent:
7798285, Sep 21, 2010
Filed:
Nov 14, 2008
Appl. No.:
12/271189
Inventors:
Song Chiou - Cerritos CA, US
Jia Yu - San Diego CA, US
Claude Hubert - Riverside CA, US
Michael Layland - Bonita CA, US
Assignee:
Rohr, Inc. - Chula Vista CA
International Classification:
F02K 1/00
F02K 1/82
F01D 21/00
F01D 25/04
F02B 77/13
F01N 1/24
E04B 1/82
B64C 1/06
B64C 1/12
B64D 33/02
B64F 1/26
US Classification:
181213, 181204, 181210, 181214, 181222, 181286, 181290, 181292, 181293, 244 53 B, 244131, 244132, 415 9, 415119
Abstract:
An acoustic inner barrel for an aircraft engine nacelle inlet is constructed from a composite material and is formed as a single, 360-degree annular segment. The barrel includes an inner skin, an outer skin, a cellular core disposed between the inner skin and the outer skin, and at least one crack and delamination stopper extending radially from the inner skin to the outer skin.

Linear Acoustic Liner

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US Patent:
7921966, Apr 12, 2011
Filed:
Aug 13, 2008
Appl. No.:
12/190805
Inventors:
Song Chiou - Cerritos CA, US
Jia Yu - San Diego CA, US
Claude Hubert - Riverside CA, US
Michael Layland - Bonita CA, US
Assignee:
Rohr, Inc. - Chula Vista CA
International Classification:
E04B 1/84
B64D 33/02
E04B 1/82
B64D 33/00
US Classification:
181292, 181288, 181214, 244538
Abstract:
A linear acoustic liner for an aircraft includes a cellular core having a first surface and an opposed second surface. A substantially imperforate back skin covers the first surface, and a perforate face skin covers the second surface of the core. The perforate face skin includes an outer face skin layer having a first plurality of spaced openings, an inner face skin layer having a second plurality of spaced openings, and a porous layer disposed between the outer face skin layer and the inner face skin layer. Each of the first plurality of spaced openings are substantially aligned with one of the second plurality of spaced openings.

Linear Acoustic Liner

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US Patent:
8196704, Jun 12, 2012
Filed:
Mar 14, 2011
Appl. No.:
13/047408
Inventors:
Song Chiou - Cerritos CA, US
Jia Yu - San Diego CA, US
Claude Hubert - Riverside CA, US
Michael Layland - Bonita CA, US
Assignee:
Rohr, Inc. - Chula Vista CA
International Classification:
E04B 1/84
B64D 33/02
E04B 1/82
B64D 33/00
US Classification:
181292, 181288, 181214, 181296, 244 53 B
Abstract:
A linear acoustic liner for an aircraft includes a cellular core having a first surface and an opposed second surface. A substantially imperforate back skin covers the first surface, and a perforate face skin covers the second surface of the core. The perforate face skin includes an outer face skin layer having a first plurality of spaced openings, an inner face skin layer having a second plurality of spaced openings, and a porous layer disposed between the outer face skin layer and the inner face skin layer. Each of the first plurality of spaced openings are substantially aligned with one of the second plurality of spaced openings.

Crack And Delamination Stoppers For Aircraft Propulsion System Components

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US Patent:
20120291416, Nov 22, 2012
Filed:
May 11, 2012
Appl. No.:
13/470049
Inventors:
Song Chiou - Cerritos CA, US
Jia Yu - San Diego CA, US
Claude Hubert - Riverside CA, US
Michael Layland - Bonita CA, US
Assignee:
Rohr, Inc. - Chula Vista CA
International Classification:
B64D 33/04
F02K 3/04
US Classification:
602262, 23926511
Abstract:
An inner fixed structure of a thrust reverser includes an inner skin, an outer skin, a cellular core disposed between the inner skin and the outer skin, and at least one crack and delamination stopper extending radially between the inner skin and the outer skin.
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Jia Wang Yu from Baldwin Park, CA Get Report